View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 00012U 59001B 18115.69782258 .00000318 00000-0 16628-3 0 9999
2 00012 32.9108 212.9563 1668118 275.6381 65.7117 11.44218789432752
| Epoch (UTC): | 25 April 2018 16:44:51 |
| Eccentricity: | 0.1668118 |
| inclination: | 32.9108° |
| perigee height: | 553 km |
| apogee height: | 3328 km |
| right ascension of ascending node: | 212.9563° |
| argument of perigee: | 275.6381° |
| revolutions per day: | 11.44218789 |
| mean anomaly at epoch: | 65.7117° |
| orbit number at epoch: | 43275 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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